公开(公告)号：US11465747B2

公开(公告)日：2022-10-11

申请号：US16527733

申请日：2019-07-31

Applicant: THE BOEING COMPANY

Inventor： Kevin Cassou ,  Gregory A. Tubbs

IPC: B64D11/00 ,  B64F5/10

Abstract: A vehicle includes an interior cabin, a primary structure within the interior cabin, a plurality of securing mounts having first ends directly coupled to the primary structure, and second ends, and an overhead support platform system directly coupled to the second ends of the plurality of securing mounts. The overhead support platform system includes at least one adapter rail having a plurality of commodity mounts. At least one commodity is directly coupled to the overhead support platform system. The commodity is adaptively secured to one or more of the plurality of commodity mounts.

公开(公告)号：USD920889S1

公开(公告)日：2021-06-01

申请号：US29695038

申请日：2019-06-14

Applicant: The Boeing Company

Designer： Gregory A. Tubbs ,  Kevin Cassou ,  David A. Young ,  Trevis Kurz ,  Franco M. Cagnina ,  Gary E. Liljebeck ,  Adam Boroughs

公开(公告)号：US10992120B2

公开(公告)日：2021-04-27

申请号：US16459499

申请日：2019-07-01

Applicant: The Boeing Company

Inventor： Colin R. Kreiger ,  Gregory A. Tubbs ,  Alexander J. Matsuoka ,  Michael E. Frick ,  Ryan P. Rogers ,  Jackson L. Fadely ,  Derrick B. Pruitt

IPC: H02G3/04 ,  B64D11/06

Abstract: There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.

公开(公告)号：US20210006051A1

公开(公告)日：2021-01-07

申请号：US16459531

申请日：2019-07-01

Applicant: The Boeing Company

Inventor： Colin R. Kreiger ,  Alexander J. Matsuoka ,  Derrick B. Pruitt ,  Michael E. Frick ,  Gregory A. Tubbs

IPC: H02G3/04 ,  H02G3/34 ,  H02G1/08

Abstract: There is provided a raceway cover assembly for installing conductive element(s) in an aircraft. The raceway cover assembly includes a raceway cover for removable coupling to a raceway. The raceway is configured for attachment to a sidewall assembly for use in a cabin of the aircraft. The raceway cover includes a first cover side, a second cover side, and retaining element(s) disposed on the first cover side. The raceway cover assembly further includes the conductive element(s) coupled and retained to the first cover side, with the retaining element(s), to form the raceway cover assembly. The conductive element(s) and the raceway cover are assembled together at a location off of the aircraft, prior to installing the raceway cover assembly with the one or more conductive elements in the aircraft, which allows for routing of the one or more conductive elements in the raceway cover at the location off of the aircraft.

公开(公告)号：US20210006050A1

公开(公告)日：2021-01-07

申请号：US16459499

申请日：2019-07-01

Applicant: The Boeing Company

Inventor： Colin R. Kreiger ,  Gregory A. Tubbs ,  Alexander J. Matsuoka ,  Michael E. Frick ,  Ryan P. Rogers ,  Jackson L. Fadely ,  Derrick B. Pruitt

IPC: H02G3/04 ,  B64D11/06

Abstract: There is provided a sidewall closeout area assembly for an aircraft. The assembly includes a raceway with a first end to attach to a sidewall assembly, a second end to attach to aircraft floor structure(s), and a raceway body with first access opening(s) providing access to one or more of, a crown area and an underfloor area, for conductive elements routed along the raceway. The assembly further includes a raceway cover removably coupled to the raceway and having second access opening(s) providing access to the cabin and to an overfloor area in the cabin for the conductive elements. The assembly further includes a closeout area formed between the raceway body and the raceway cover, to house and protect the conductive elements. The assembly facilitates accessibility to the conductive elements, and provides a routing path for the conductive elements that does not need to be reconfigured for different aircraft cabin layouts.

公开(公告)号：US20170129581A1

公开(公告)日：2017-05-11

申请号：US14935788

申请日：2015-11-09

Applicant: THE BOEING COMPANY

Inventor： Thomas Seth Perkins ,  Cory Michael Hitchcock ,  John Erik West ,  Adam R. Weston ,  Gregory A. Tubbs

IPC: B64C1/06 ,  B64C1/18 ,  B64C1/40

CPC classification number: B64C1/066 ,  B64C1/40 ,  B64C2001/009 ,  Y02T50/46

Abstract: A return air bridge for use in an aircraft assembly includes an inboard portion configured to couple to a sidewall assembly at a bottom edge of the sidewall assembly and an outboard portion configured to couple to a structural member. The return air bridge also includes at least one support coupling the inboard portion to the outboard portion such that a return air flow path is defined between the inboard portion and the outboard portion. The outboard portion comprises a plate configured to direct an air flow along the return air flow path upwardly with respect to the bottom edge of the sidewall assembly.

公开(公告)号：US09580955B2

公开(公告)日：2017-02-28

申请号：US14942966

申请日：2015-11-16

Applicant: The Boeing Company

Inventor： Gregory A. Tubbs

IPC: E04B1/346 ,  E06B3/50 ,  E06B7/28 ,  E05D15/26 ,  E06B3/48 ,  B64D11/02 ,  E06B3/34 ,  E04B2/74

CPC classification number: E06B3/5072 ,  B64D11/02 ,  E04B2/7407 ,  E05D15/26 ,  E06B3/34 ,  E06B3/48 ,  E06B3/481 ,  E06B3/486 ,  E06B3/5054 ,  E06B7/28 ,  E06B2003/343

Abstract: The present disclosure is generally directed to a method of operation for a convertible door system including a door accessible compartment having a moveable dividing wall that substantially divides the compartment into a first and a second sub-compartment. A first door assembly, configured to allow access to the first sub-compartment, is disposed between a first of two opposing sidewalls and the moveable dividing wall. A second door assembly, configured to allow access to the second sub-compartment, is disposed between a second of the two opposing sidewalls and the moveable dividing wall. A first and a second hinge assembly are adapted to rotationally join the first and second door assembly to respective opposing sidewalls. A third hinge assembly is adapted to rotationally join the moveable dividing wall to either the first door assembly or the second door assembly.

Abstract translation: 本公开总体上涉及一种用于可转换门系统的操作方法，该可转换门系统包括具有可移动分隔壁的门可接近室，其基本上将隔室分成第一和第二子隔室。 构造成允许进入第一子隔间的第一门组件设置在两个相对侧壁中的第一侧壁和可移动分隔壁之间。 构造成允许进入第二子隔间的第二门组件设置在两个相对的侧壁中的第二侧壁和可移动分隔壁之间。 第一和第二铰链组件适于将第一和第二门组件旋转地连接到相应的相对侧壁。 第三铰链组件适于将可移动分隔壁旋转地连接到第一门组件或第二门组件。